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At a glance
AGM-179 JAGMlarger figure on 0 of 2
Astra (missile)larger figure on 2 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source70 in (1,778 mm)[source]
Length
Single sourceConfiguration
| Specification | AGM-179 JAGM | Astra (missile) |
|---|---|---|
| Speed | — | Mk-1: Mach 4.5[source] |
| Type | Air-to-surface missile[source] | Beyond-visual-range air-to-air missile[source] |
| In service | Achieved IOC March 1st 2022 with the U.S. Marine Corps[source] | 2019 ( 2019 ) –present[source] |
| Manufacturer | Lockheed Martin[source] | Bharat Dynamics Limited[source] |
3.84 m (12.6 ft)[source]
Warhead weight
Single source15 kg (33 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Unit cost | US$319,000 (FY 2023)[source] | Mk-1: ₹ 7−8 crore (US$−830,000)[source] |
|---|
| No. built | 26,319 (planned)[source] | — |
|---|
| Guidance system | Semi-active laser and millimeter-wave radar[source] | Mid-course: FOG - INS + Mid-course update via datalink Terminal: ARH[source] |
|---|
| Launch platform | Helicopters and fixed-wing aircraft[source] | Su-30MKI MiG-29K Tejas Mk.1/1A MiG-29UPG (Trial-phase) HAL Tejas Mk2 (Planned) AMCA (Planned) TEDBF (Planned) Rafale Marine (Planned)[source] |
|---|
| National origin | United States[source] | — |
|---|
| Place of origin | — | India[source] |
|---|
| Used by | — | Indian Air Force Indian Navy[source] |
|---|
| Wars | — | 2025 India–Pakistan conflict[source] |
|---|
| Designer | — | Defence Research and Development Laboratory ( DRDO )[source] |
|---|
| Produced | — | 2017 − Present[source] |
|---|
| Variants | — | Mk-1 (Operational) Mk-2 (LSP) Mk-3 (Trial-phase) VL-SRSAM (Trial-phase)[source] |
|---|
| Warhead | — | High-explosive pre- fragmented HMX / PU[source] |
|---|
| Detonation mechanism | — | Mk-1: Radio proximity fuze Mk-2: Optical proximity fuze[source] |
|---|
| Engine | — | Mk-1: Solid-propellant rocket Mk-2: Dual-thrust pulsed rocket motor Mk-3: Solid Fuel Ducted Ramjet[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight ceiling | — | 20 km (66,000 ft)[source] |
|---|